doi: 10.3389/fmats.2018.00022

Edited by:
*Alberto Corigliano,*
*Politecnico di Milano, Italy*
Reviewed by:
*Marco Miniaci,*
*Georgia Institute of Technology,*
*United States*
*Massimiliano Gei,*
*Cardiff University, United Kingdom*
*Correspondence:
*Ada Amendola*
*adaamendola1@unisa.it*

Specialty section:
*This article was submitted to*
*Mechanics of Materials,*
*a section of the journal*
*Frontiers in Materials*
*Received: 16 February 2018*
*Accepted: 28 March 2018*
*Published: 17 April 2018*
Citation:
*Amendola A, Favata A and*
*Micheletti A (2018) On the Mechanical*
*Modeling of Tensegrity Columns*
*Subject to Impact Loading.*
*Front. Mater. 5:22.*
*doi: 10.3389/fmats.2018.00022*

### On the Mechanical Modeling of

### Tensegrity Columns Subject to

### Impact Loading

Ada Amendola1_{*, Antonino Favata}2_{and Andrea Micheletti}3

*1 _{Department of Civil Engineering, University of Salerno, Fisciano, Italy,}2_{Department of Structural and Geotechnical}*

*Engineering, Sapienza University of Rome, Rome, Italy,3 _{Department of Civil Engineering and Computer Science Engineering,}*

*University of Rome Tor Vergata, Rome, Italy*

A physical model of a tensegrity columns is additively manufactured in a titanium
alloy. After removing sacrificial supports, such a model is post-tensioned through
suitable insertion of Spectra® _{cables. The wave dynamics of the examined system is}

first experimentally investigated by recording the motion through high-speed cameras assisted by a digital image correlation algorithm, which returns time-histories of the axial displacements of the bases of each prism of the column. Next, the experimental response is mechanically simulated by means of two different models: a stick-and-spring model accounting for the presence of bending-stiff connections between the 3D-printed elements (mixed bending-stretching response), and a tensegrity model accounting for a purely stretching response. The comparison of theory and experiment reveals that the presence of bending-stiff connections weakens the nonlinearity of the wave dynamics of the system. A stretching-dominated response instead supports highly compact solitary waves in the presence of small prestress and negligible bending stiffness of connections.

Keywords: tensegrity columns, wave dynamics, additive manufacturing, experimental testing, stick-and-spring structure, solitary waves

### 1. INTRODUCTION

The dynamics of acoustic metamaterials has been intensively investigated over recent years, with the aim of designing unconventional mechanical devices like acoustic band gap materials, shock protectors, acoustic lenses, and energy trapping containers, to name just a few examples (refer, e.g., toLu et al., 2009; Craster and Guenneau, 2013; Theocharis et al., 2013; Hussein et al., 2014; Leonard et al., 2014; Chronopoulos et al., 2017; Claeys et al., 2017; Harne et al., 2017; Ponge et al., 2017; Tallarico et al., 2017; Miniaci et al., 2018and references therein). It has been shown that engineered metamaterials may find application for protecting materials and structures against impacts with external objects (Fraternali et al., 2010; Mitchell et al., 2014), as well as for the design of sound-focusing devices (Spadoni and Daraio, 2010), the manufacturing of noninvasive sensors and actuators for structural health monitoring (Ngo et al., 2012; Rizzo et al., 2014), and the fabrication of novel seismic protection devices (Brûlé et al., 2014; Kr¨ödel et al., 2015; Miniaci et al., 2016; Colombi et al., 2017; La Salandra et al., 2017).

Lattice structures obtained by assembling tensegrity units, such as T3 tensegrity prisms (Skelton and de Oliveira, 2010), exhibit a mechanical response that can be continuously varied from hardening to softening, by changing the geometrical, mechanical, and prestress parameters (Fraternali et al., 2012, 2014a,b; Amendola et al., 2014, 2015; Rimoli, 2016; Montuori and Skelton, 2017; Rimoli and Pal, 2017). The geometrically nonlinear response of

Amendola et al. Tensegrity Columns Subject to Impact Loading

a tensegrity system is caused by the presence of one or more infinitesimal mechanisms, i.e., sets of nodal displacements causing second-order member elongations, owing to the fact that the equilibrium operator is singular in the considered configuration (Calladine, 1978; Calladine and Pellegrino, 1991; Micheletti, 2012; Fraternali et al., 2015; Modano et al., 2018). Recent studies (Fraternali et al., 2012, 2014b) have revealed that tensegrity columns composed of T3 prisms are suitable for use as acoustic lenses supporting extremely compact solitary waves.

In this work, we experimentally test the dynamic response of a tensegrity column subjected to impact loading, and correspondingly we perform numerical simulations of the examined tests using two different elastic models, respectively described in Favata et al. (2014) and Davini et al. (2016). An additive manufacturing (AM) technique based on Electron Beam Melting (EBM) is employed to build all the elements of the tested structure, except for the cables, which are subsequently added to the 3d-printed structure through a post-tensioning technique (Amendola et al., 2015). The mechanical modeling of such a structure is first analyzed through the stick-and-spring model presented inFavata et al. (2014), which takes into account that the nodes of the 3D-printed structure form bending-stiff connections. It models the system by considering bars and bases to be inflexible, by describing the cables as linear springs, and attaching angular springs to the nodes (mixed bending-stretching response). The second examined model (Davini et al., 2016) is instead a pure tensegrity model that introduces frictionless pin-connections between elements, describes the cables as linear springs, and models the bars and the bases of the prisms as rigid bodies (purely stretching response). Other than comparing for the first time the experimental impact response of a tensegrity column to the numerically predicted response of the above models, this work highlights differences and similarities between such models, providing useful directions for the design of tensegrity metamaterials with sound-focusing abilities.

### 2. EXPERIMENTAL SETUP

We experimentally investigate the dynamic response of a 3D-printed physical model of a tensegrity column (Amendola et al., 2015) under impact loading. Such structure consists of ten regular tensegrity prisms with triangular bases (T3 prisms) (Skelton and de Oliveira, 2010) superposed to each other.

**Figure 1A** shows the tested column partly manufactured in
Ti6Al4V titanium alloy using the EBM technique (Amendola
et al., 2015) and the computer-aided design (CAD) model drawn
**in Figure 1B. The Arcam S12 EBM facility at the Department of**
Materials Science and Engineering, University of Sheffield was
employed to manufacture the examined structure, by depositing
layers of Ti6Al4V powder with minimum feature size down to 0.4
mm (Tammas-Williams et al., 2015).

Each T3 prism of the column is left-handed, i.e., the upper
base is rotated counter-clockwise with respect to the bottom
base by an angle of 5π/6 about the prism’s axis1 _{(cf.} _{Davini}
et al., 2016). Each T3 prism is made by three bi-conical bars

1_{When a T3 prism is right-handed the base is rotated clockwise by the same angle.}

connected to the vertices of two triangular plates with thickness
t through spherical nodes with 3 mm diameter. These elements
are 3D-printed together with the aid of additional sacrificial
linear elements which are mechanically removed afterward.
Three strings elements (or cables) made of Spectra_{
}R _{fibers are}

then added to each prism on using the post-tension technique
illustrated inAmendola et al. (2015). The geometric properties of
**a prism are given in Table 1. The symbols s**N, bN, and hNdenote

respectively the length of the edges of the base plates, the length
of the bars, and the height of the prism (measured as the distance
between the base centers) (Amendola et al., 2015**) (cf. Figure 1B).**
The maximum and minimum diameters of the bars are denoted
by D and d, respectively.

An in-house experimental setup is designed and assembled to
apply an impact load to the top base of the column, while keeping
the bottom base fixed to an aluminium plate. The strings of the
structure are pre-stretched by passing them through bridge pins
**applied to the aluminum plate (Figure 1A). A vertical thin rod**
passing through the units was inserted in order to stabilize the
column and prevent possible bending modes.

The top base of the columns is impacted by a spherical
striker with 5 g mass made of Polytetrafluoroethylene (PTFE)
**(Figure 1A), which falls with null initial velocity for 0.5 m in a**
duct delimited by four Teflon tubes. The motion of the column
produced by the impact with the striker is recorder through
two high-speed cameras FASTCAM Mini UX100, and the axial
(vertical) displacements of the upper base of each unit are
measured using a Digital Image Correlation technique (Deng
et al., 2017; Schaeffer et al., 2017). Such a technique employs
image acquistion with a rate of 4,000 fps at 1,280 × 1,024 pixel
resolution, and the triggering of the striker downfall through a
precision screw, in order to obtain a repeatable perturbation of
the impacted base (Nadkarni et al., 2016).

### 3. STICK-AND-SPRING MODEL

The EBM technique described in section 2 does not allow for the realization of spherical hinges between bars and base plates of the tensegrity column; on the contrary, the nodes of the 3D-printed structure provide bending-stiff connections between such elements. This observation leads us to employ a stick-and-spring (S&S) model (Favata et al., 2014) to describe the dynamic response of the physical model under examination.

A S&S structure is a collection of nodes, edges, and wedges:
edges are imagined as node-to-node inflexible but extensible
straight sticks, acting as axial springs when extended; wedges
are imagined as complexes of two sticks sharing one end node,
equipped by an angular spring reacting to relative rotations of the
two wedge sticks in their common plane. A S&S structure differs
from a tensegrity structure because, owing to the presence of
angular springs, edges are subjected to shear forces and bending
**moments, in addition to axial forces (see Figure 1C).**

### 3.1. Model Description

The combinatorial description of a S&S structure is given by
the tripletS _{= (}N_{,}E_{,}W_{) consisting of: (i) a collection}N _{of}

FIGURE 1 | The tensegrity column under test (A), CAD model of a single prism (B), and sketch of a portion of the model showing also the angular springs associated to the wedges of the S&S structure (C).

TABLE 1 | Geometrical properties of a T3 prism.

t sN bN hN D d

(mm) (mm) (mm) (mm) (mm) (mm)

1.0 34.08 44.06 22.29 3.0 0.5

(ii) a collectionE_{of edges, that is, two-elements subsets of}N_{; (iii)}

a collectionW _{of wedges, that is, three-elements subsets of}N_{.}

We say that ij ∈E_{is the edge connecting nodes i, j ∈}N_{, and that}

ijk ∈W_{, with i, j, k ∈}N_{, is the wedge with head node i and tail}

**nodes j and k. We denote by p**ithe referential position vector of

**the typical node i with respect to a chosen origin point, by u**iits

**displacement, and by q**i:**= p**i**+ u**iits current position vector.

We denote the change in length of edge ij, with ℓij = ij, and

the change in angle of wedge ijk, with θijk = bjik by δℓijand δθijk,

respectively. The corresponding linearized length variations are:

δℓij**= b**ij**· u ,** δθijk**= b**ijk**· u ,** (1)

**where u is the string of nodal-displacement vectors, [u] =**
**[. . . , u**i**, . . .], while b**ij**, b**ijkare vectors depending on referential

**nodal positions p**i, i ∈ N (see Favata et al., 2014 for

details). On denoting by η the string of strain components, [η] =. . ., δℓij, . . . | . . . , δθijk, . . .

, relations (1) can be given the following compact form:

η**= Bu,** (2)

**where the linear mapping B is the kinematic compatibility**
**operator. We denote by f and χ respectively the string of**
nodal-force vectors and the string of stress measures conjugated

with η. With this notation, the balance equations can be written as:

**f = Aχ,** (3)

**where A = B**Tis the equilibrium operator.

Next, let the (positive) spring constants κijand λijkcharacterize

the linear elastic response of edge and wedge springs, respectively,
so that the elastic energy stored in a S&S structure can be written
as:
U_{=} 1
2
X
ij∈E
κij(ℓij− ℓij)2+
X
ijk∈W

λ_{ijk}(θijk− θijk)2

, (4)

with ℓijand ℓijthe current length and the rest length of the axial

spring on edge ij, while θijkand θijkare the current angle and the

rest angle of the angular spring on wedge ijk. On introducing the kinetic energy:

K** _{(q, ˙q) =}** 1

2**˙q · M(q)˙q,** (5)

**with M a diagonal mass operator corresponding to lumped nodal**
masses, the nonlinear motion equations are given by:

**M ¨q + eA _{(q)χ (q) = 0,}** (6)

where e**A(q) is the equilibrium operator in the current placement.**
This equation can be linearized about an equilibrium placement

**q**_{0}, obtaining:

Amendola et al. Tensegrity Columns Subject to Impact Loading

**where K**T := ∂**q**2Uis the tangent stiffness operator2.

The response of the tensegrity column under impact loading is obtained through numerical integration of (6) and (7) subject to assigned initial conditions.

### 3.2. Simulation of Impact Tests

The impact test was simulated by means of the S&S model under the following assumptions.

• Cables are modeled as edges, with stiffness κc = Ecπd2c/(4lc),

where Ec is the Young modulus, dc the diameter, and lc =

l2_{b}− 2√3a21/2is the current length of the cables, with lbthe

length of the bar and a the base radius; • Cable prestress is considered to be negligible3;

• Bars are modeled as edges with stiffness κb = Ebπd2_{b}/(4lb),

where Ebis the Young modulus and dbthe diameter;

• Each triangular base is modeled as three pin-jointed bars of stiffness κbforming the triangle;

• Wedges are considered between base triangles and bars (see

**Figure 1B**_{, right), their stiffness is λ = ακ}bl2c, with α a

dimensionless parameter measuring the relative importance of edge-stretching and wedge-opening (Favata et al., 2014), which in the present study is fitted with the experimental results; • Nodal masses m are assigned by subdividing the total

measured mass of the structure, 53.0 g into 3 (vertices) × 10 (bases) = 30 equal parts.

• As initial value of the downward velocity we assumed v0 =

2 m/s, by averaging measurements during a short time interval after impact. We also assumed that the impact cause the top base to have an initial angular velocity about the prism’s axis given by ω0 = 2hNv0/a2 ≃ 0.2304 rad/s, with a =

√
3 sN/3,
2_{See}_{Favata et al. (2014)}_{for a detailed expression of K}

T.

3_{We checked that, owing to the small axial stiffness of cables, a modest prestress}

does not change results significantly.

so that the top base initially moves along the infinitesimal mechanism of the top prism (Fraternali et al., 2014a).

**Table 2** summarizes the adopted values of the S&S modeling
parameters.

The stiffness of wedge springs, controlled by the dimensionless parameter α, is assigned by matching the time t at which the top base returns to the initial position (subsequently continuing its upward motion). In the experiment, t = 18.9892 ms; in the simulation, the same value is found when α = 6.0655 · 10−4. We observe a good agreement between oscillation amplitudes in the two cases.

**Figure 2** shows a comparison on the displacements of the
prisms #2, #4, #6, #8, #10 (top prism), between experimental
results (dotted line) and numerical results (solid line). Numerical
results are obtained by integrating the nonlinear equation of
**motion (6). Figure 3A shows a comparison on the displacements**
of the first and the last prism, between experimental results
(dotted line), results obtained by numerical integration of both
the nonlinear equation of motion (6) (solid line), and those
obtained from the linearized equation of motion (7) (dashed
**line). Figure 3B shows numerical results for the axial strain of the**
first and last prism, which is defined as the relative displacement
between the two bases of a prism, divided by hN. Experimental

results display larger oscillations, in particular for the top prism.

TABLE 2 | Model parameters.

*Ec* 5480 MPa
*dc* 0.1 mm
*lb* 44.06 mm
*Eb* 110 · 103MPa
*db* 1.75 mm
*hN* 22.29 mm

FIGURE 3 | (A) Displacements of the top and bottom base, comparison between experiments (dotted line) and numerical simulations with nonlinear theory (solid line) and linearized theory (dashed line) of the S&S model. (B) Axial strains in the top and bottom prism obtained with nonlinear theory (solid line) and linearized theory (dashed line).

*TABLE 3 | First maximum value of the displacement umax*and correspondent
*time tmax*.

Top prism Exper. Nonlin. th. Lineariz. th.

*u*max(mm) −1.7812 −1.8004 −1.9344

*t*max(ms) 1.75 1.70 1.70

Bottom prism Exper. Nonlin. th. Lineariz. th.

*u*max(mm) −0.7506 −1.2495 −1.4079

*t*max(ms) 10.0 10.0 10.1

In this regard, we observed that in the experiment triangular bases do not remain perfectly horizontal during the motion, and this is likely to be the reason of the larger oscillations in the measured displacement. The first maximum value of the displacement umaxand the correspondent time tmaxis reported

**in Table 3. It is worth noting that, by looking at Table 3 and**

**Figure 2**, the response in the linearized case is close to that in
the nonlinear case.

### 4. PURE TENSEGRITY MODEL

Both simulations and experimental results presented in the previous section show that the mixed bending-stretching regime produces a not localized wave transmission response of the tensegrity column under examination. In this section, we propose some possible directions toward the design of a device with more “focused” dynamic response under impact loading in the pure stretching regime. In order to do this, we adopt the simpler, pure tensegrity model presented inDavini et al. (2016), where the Lagrange’s equation of motion of a tensegrity column are solved numerically. The assumptions of this model are the following ones: only cyclic-symmetric motions with respect to the column’s axis are considered; nodes are frictionless hinges

between connected elements; all bars are rigid and massless;
cables are linearly elastic and massless. In our case, each
triangular base is a rigid body with a mass 3 m and moment of
inertia 3 m a2_{.}

We investigated the following three cases.

**CASE1** — We considered cable stiffness to be the same as in
the present S&S model. Then we determined the cable
prestrain by matching the time t at which the top base
returns to the initial position with that measured during
the experiment. By doing so, the resulting prestrain takes
the unrealistic value of 85%. The results are shown in

**Figure 4**(dashed line) , where it is possible to see a linear
behavior similar to that of the mixed bending-stretching
response.

**CASE2** — We assign the more realistic value of 5% to
the prestrain and determine the cable stiffness by
matching the time t with that of the experiment.
The resulting cable stiffness is 15.5 times higher
than that of the original structure. Results are shown
**in Figure 4 (dash-dot line), where we still observe a**
response similar to that of the mixed bending-stretching
regime.

**CASE3** — We assign a low prestrain to cables, equal to 1% and,
again by matching the time t with that of the experiment,
we determine the stiffness of cables to be 55.5 times higher
than that of the original structure. The results are shown in

**Figure 4**(solid line), which displays a much more marked
nonlinear response4_{.}

It is worth noting that the above cases refer to models of tensegrity columns different from that experimentally tested

4_{This is highlighted for example by the different amplitudes in tension and}

**compression of the bottom prism (Figure 4B, solid line), owing to a stiffer response**
in tension.

Amendola et al. Tensegrity Columns Subject to Impact Loading

FIGURE 4 | Displacements of top prism (A) and bottom prism (B): experiments (dotted line), Case 1 (dash-dot line), Case 2 (dashed line), and Case 3 (solid line) of the pure tensegrity model.

FIGURE 5 | Snapshot at 65 ms of prism strains along a column composed by 100 prisms. Nonlinear Stick-and-Spring model (A). Pure tensegrity model: Case 1 (B); Case 2 (C), and Case 3 (D).

in the present work (experimental model), and they are here
presented with the aim of exploring the nonlinear potential of the
**wave dynamics of pure tensegrity lattices. The results in Figure 4**
show that the tensegrity models of Cases 1 and 2 reproduce
fairly well the displacement vs. time response of the experimental
model, while there are larger differences with Case 3.

For a better visualization of nonlinear effects, we repeated
the simulations on a column composed of 100 units, and we
**represented in Figure 5 the strain of each prism of the column**
**at a fixed time (t = 65 ms). In all the results shown in Figure 5**
we observe the formation of a leading compression strain pulse
followed by an oscillatory tail. By comparing Cases 1–3 and the

Stick-and-Spring model analyzed in Sect. 3 (nonlinear theory),
we observe that for Case 3 (when the cross-cable prestrain is
1%) the deformation of the column is more localized at the wave
front, since in this case the amplitude of the leading compression
strain pulse is much larger than that of the oscillatory tail, and is
**more markedly separated from the tail (Figure 5D), as compared**
**to Cases 1–2 (Figures 5B,C) and the Stick-and-Spring model**
**(Figure 5A).**

### 5. CONCLUSION AND FUTURE WORK

### 5.1. Concluding Remarks

We have performed an impulsive dynamic test on a physical model of a tensegrity column, on comparing the measured displacements to those computed numerically through two different models: a stick-and spring model accounting for bending deformation of the nodes (Favata et al., 2014), and a pure tensegrity model accounting for a pure-stretching response of all the members of the system (Davini et al., 2016). The first model is intended to capture the experimental response of the analyzed physical model, while the second one is aimed at providing directions for the design of alternative systems featuring highly nonlinear dynamic response. The given results show a fairly good agreement between measurements and simulations performed with the first model. The second model is also able to reproduce the response observed during the experiment when one prescribes a suitable prestrain to the cables, since such a property significantly influences the axial stiffness of the units (Fraternali et al., 2014a). We have observed that bending-stiff nodal connections, a feature of the 3D-printed structure due to the not-negligible size of the junctions, may greatly reduce nonlinearities in the response of tensegrity lattices. We found that a similar effect can also be obtained in the second model by fictitiously raising the prestress level. This behavior can be explained by considering that the tangent stiffness of the tensegrity lattice is the sum of a material contribution (owing mainly to the stiffness of angular springs) and a geometric contribution (owing to prestress) (Favata et al., 2014). In relation to this, we observed also that a more marked nonlinear behavior occurs for smaller prestress levels and smaller values of the stiffness of angular springs.

### 5.2. Future Work

The results of the present study highlight that a pure tensegrity behavior with negligible bending deformation of the nodes and low prestress may lead to design novel metamaterials that enable unconventional wavefocusing methodologies based on the

propagation of localized stress/strain waves, whose support is concentrated in narrow regions of space. This obviously calls for the adoption of manufacturing techniques that are able to build perfect hinges at the nodes, such as e.g. the multiscale AM techniques described in Meza et al. (2014); Zheng et al. (2014). Arrays of tensegrity columns with stretching-dominated response may be employed to fabricate tunable focus acoustic lenses whose working principle is based on the propagation of localized stress waves, whose support can be adjusted through the control of the global precompression of the structure, and/or the prestretch of the cables forming the units. On applying different levels of prestress to such metamaterials, one can be able to generate compact stress waves with different phases within the system, which are expected to interact at a focal point in an adjacent medium (i.e., a material defect to be targeted) (Spadoni and Daraio, 2010). We address specific studies on such engineering applications of tensegrity lattices to future work, with the aim of designing and manufacturing novel acoustic lenses, and innovative sensors/actuators for monitoring structural health and damage detection in materials and structures (Rizzo et al., 2014).

### AUTHOR CONTRIBUTIONS

AA run the experiments at the Department of Mechanical and Process Engineering, ETH Zurich, on occasion of an internship under the supervision of Prof. Chiara Daraio. AM led the formulation and implementation of the tensegrity model and contributed to the formulation of the stick-and-spring model. AF led the formulation and implementation of the stick-and-spring model and contributed to the formulation of the tensegrity model. All the authors collaborated on the writing of the manuscript.

### ACKNOWLEDGMENTS

The authors wish to thank Evert Hernández-Nava, Christopher Smith, Russell Goodall, and Ian Smith for their support and advice during the manufacturing of the Ti-6Al-4V models at the Department of Materials Science and Engineering, University of Sheffield, UK. The authors are also grateful to Chiara Daraio for providing continuous support and advice during the experimental tests, which were run at the Department of Mechanical and Process Engineering of ETH Zurich. AF acknowledges the financial support of Sapienza University of Rome (University Grants 2016 and 2017).

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**Conflict of Interest Statement:** The authors declare that the research was

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